FIELD OF THE INVENTION
[0001] The present invention relates to a metallic member, especially, aluminum, ferrous
and copper alloys, having one or more of high electric conductivity, high thermal
conductivity, heat resistance and wear resistance, in which super fine ceramic particles
and solid lubricant particles or solid lubricant short size fibers, especially, graphite
whiskers, are dispersed, and is more particularly concerned with a nitride dispersion
strengthening copper alloy, a nitride dispersed aluminum alloy and a nitride dispersion
strengthened iron which are suitable for use in electro-conductive, heat-resistant
strengthened members such as sliding contact members and electric contacts, a manufacturing
method thereof, and use thereof.
TECHNICAL BACKGROUND
[0002] For the purpose of utilizing advantageous basic characteristics of copper, i.e.,
high electric conductivity and high thermal conductivity, in various industrial products,
many copper alloys improved to overcome a weak point of copper, i.e., a deficiency
in strength, have been manufactured. As methods for strengthening copper, known hitherto
are a method of adding one or more of elements having less solubility into matrix,
such as Zr, Cr, Cd and Be, to develop precipitation hardening by aging treatment,
and a method of dispersing ceramic particles, which are hard to react with a copper
matrix phase, into the matrix phase. The strengthening is effected by precipitates
or ceramic particles which are finely dispersed in the mother phase and prevent dislocation
movement responsible for a plastic deformation. The former strengthening method is
disclosed in JP-A-57-9850. Of the latter strengthening method, oxide-dispersion-hardening
is disclosed in JP-A-2-213433, carbide-dispersion-hardening in JP-A-1-96338, and nitride-dispersion-hardening
in JP-A-60-208402, etc.
[0003] Meanwhile, addition of graphite powder or BN powder improves lubrication property,
low contact resistance and seizure resistance of copper alloys. A method for manufacturing
such copper alloys is disclosed in, for example, JP-A-57-123943. Addition of graphite
powder is practiced to manufacture copper alloys for electric contacts, aiming at
an improvement in low contact resistance and seizure resistance, and is disclosed
in JP-A-62-284031.
[0004] The aforesaid precipitation-hardening copper alloy can keep the strength at temperatures
of about 400°C or below, but loses its hardening ability at temperatures higher than
400°C due to pyrolysis of precipitates.
[0005] On the other hand, as dispersing methods used to manufacture a ceramic dispersion
strengthening copper alloy, known hitherto are an oxide dispersion strengthening method
using a powder mixing process or an internal oxidation process, and a mechanical alloying
process adapted for a mixture of copper and fine ceramic powders as disclosed in JP-A-3-2338,
JP-A-2-213433 and JP-A-63-83240. For the fine dispersion of ceramic particles, the
internal oxidation process and the mechanical alloying process are superior. As methods
for manufacturing members made of strengthening copper alloys, there has been utilized
powder metallurgical methods such as thermal extrusion.
[0006] Taking copper as an example, if impurities are present in copper, those impurities
cause scattering of conduction electrons, thereby deteriorating high electric conductivity
and high thermal conductivity both inherent to copper. Strength of copper members
is required to be increased for enabling them to be widely used as practical materials
for industrial purposes, but any methods of strengthening copper by alloying necessarily
deteriorate the above inherent characteristics. In a precipitation-hardening copper
alloy, particularly, besides a limit in the application temperature as mentioned before,
electron scattering occurs due to strains of lattices around the precipitates and
changes in electron states around a trace amount of residual metallic solute atoms,
making it very difficult to expect high electric conductivity and high thermal conductivity
comparable to those of pure copper.
[0007] Although increasing the strength of copper while maintaining excellent characteristics
thereof is quite difficult, an optimum method for solving this problem is the above-mentioned
method of dispersing ceramic particles which are less reactive with copper.
[0008] Al₂O₃ has been most widely employed as dispersion strengthening particles for copper,
and an Al₂O₃ dispersion strengthened copper alloy has been manufactured for commercial
marketing. Of methods for manufacturing that strengthened copper alloy, however, an
internal oxidation process of a polycrystalline powder of a copper-aluminum low alloy
has the problem of deteriorating the strength at high temperatures because coarse
Al₂O₃ are formed at grain boundaries.
[0009] On the other hand, an Al₂O₃ dispersion strengthened copper alloy manufactured by
a step of mechanical alloying of mixture of copper powder and fine Al₂O₃ powder, or
steps of mechanical alloying to mixture of fine copper oxide powder and fine Al₂O₃
powder and reducing it, and a subsequent step of sintering the alloy exhibits the
superior strength. However, increasing the amount of Al₂O₃ added to enhance the strength
leads to an increase in the content of copper oxide in the copper matrix phase, thus
resulting in deterioration of electric conductivity and thermal conductivity. This
phenomenon occurs in common to those alloys using ceramic oxides as dispersion powder.
As to the reasons, it is believed that during sintering of copper particles and oxide
particles, an reaction occurs at contact interface therebetween to form thin copper
oxide films on the copper particles, and deformations developed with progress of the
sintering cause exfoliation and dispersion of the copper oxide. In the case of utilizing
an oxide dispersed copper alloy as a stabilizer for metallic superconductor coils,
especially, care must be paid so as to maintain a high degree of purity of copper
matrix phase.
[0010] Further, during reducing heat treatment in which a large amount of copper oxide and
Al₂O₃ particles after the mechanical alloying are reduced at temperatures of 1065°C
or below in the above manufacturing steps, the treatment temperature is hard to control
because of an exothermic reaction between hydrogen and the copper oxide, making it
very difficult to determine whether reduction from the copper oxide to copper has
been completed or not over the entirety of powder. If the reducing reaction is incomplete,
the content of oxygen remaining in the matrix would be increased, with the result
of deteriorating the excellent characteristics of copper.
[0011] Ceramic dispersion particles are more or less bonded to the matrix phase, and impurities
in the ceramic dispersion particles penetrate into the matrix phase during the mechanical
alloying and through the interface reaction during the sintering, thereby contaminating
the matrix phase. Accordingly, utilization of high purity ceramic particles is desired.
It can be also said that a copper alloy in which are dispersed those ceramic particles
having at least one of excellent copper characteristics, i.e., high electric and high
thermal conductivities, and being hard to react with copper, is suitable as the ceramic
dispersion strengthening copper alloy.
[0012] Meanwhile, in conventional copper alloys for use as wear-resistant materials, graphite
or BN having superior lubrication property has been generally added. In view of practical
application of graphite to electric contacts, especially, it is believed that wear-resistant
contact materials exhibiting superior characteristics to conventional copper alloys
can be developed by using such graphite as having excellent strength and thermal properties.
SUMMARY OF THE INVENTION
[0013] With a view of overcoming the above-mentioned problems in prior art strengthened
copper, aluminum and ferrous alloys, and problems in prior art oxide dispersion strengthened
copper alloys, an objective of the present invention resides in providing a metallic
member having wear resistance and high strength such as suitable for use in resistance
electrodes, sliding contact members, electric contacts, a manufacturing method thereof,
and use thereof.
[0014] The present invention relates to a ceramic-particle-dispersed metallic member in
which ceramic super fine particles and solid lubricant particles or solid lubricant
short size fibers are dispersed, wherein the mean grain size of the ceramic super
fine particles is smaller than the mean grain size of the solid lubricant particles
or the mean diameter of the short size fibers, the metallic member being of a sintered
body.
[0015] Also, the present invention relates to the ceramic-particle-dispersed metallic member,
wherein the mean grain size of the ceramic super fine particles is not more than 200
nm, and the means grain size of the solid lubricant particles or the mean diameter
of the short size fibers is in the range of 0.25 to 10 µm, the metallic member being
of a sintered body.
[0016] Further, the present invention relates to the ceramic-particle-dispersed metallic
member, wherein the mean grain size of the ceramic super fine particles is not more
than 200 nm, and a region where the ceramic super fine particles are dispersed not
less than 500 in number per section area of one square micrometer is formed substantially
over the entirety region of the metallic member.
[0017] Still further, the present invention relates to the ceramic-particle-dispersed metallic
member, wherein the ceramic super fine particles have the content not more than 1
wt% and the mean grain size not more than 200 nm, and a region where the ceramic super
fine particles are dispersed not less than 500 in number per section area of one square
micrometer at 1 wt% is formed substantially over the entirety region of the metallic
member.
[0018] Still further, the present invention relates to the ceramic-particle-dispersed metallic
member, wherein the ceramic super fine particles have the content not more than 1
wt% and the mean grain size not more than 200 nm, and a region where the ceramic super
fine particles are dispersed not less than 500 in number per section area of one square
micrometer is formed substantially over the entirety region of the metallic member.
[0019] Still further, the present invention relates to the ceramic-particle-dispersed metallic
member, wherein the ceramic super fine particles have the content not more than 1
wt% and the mean grain size not more than 200 nm, and when a relationship between
the content (wt%) and the mean particle spacing (nm) of the ceramic super fine particles
is plotted in a logarithmic scale, the relationship is distributed within the rectangular
region defined by straight lines interconnecting a point A (0.01 %; 20 nm), a point
B (0.01 %; 500 nm), a point C (1.0 %; 50 nm) and a point D (1.0 %; 2 nm).
[0020] Still further, the present invention relates to the ceramic-particle-dispersed metallic
member wherein ceramic super fine particles and graphite whiskers are dispersed in
copper, aluminum or iron, and the metallic member is of a sintered body.
[0021] The present invention is also effective in the following forms relating to combinations
of matrix materials and ceramic particles, besides the above metallic members.
1) A high purity or heat-resistant nitride dispersion strengthening copper alloy consisting
of a matrix made of one selected from the group of high purity copper, copper, high
thermal-conductive copper containing graphite whiskers, and a copper alloy, and one
or two kinds of ceramic particles dispersed in matrix phase to improve the strength
of the matrix for providing the higher strength. A grain size distribution of the
dispersed ceramic particles is preferably 0.001 µm to 0.2 µm. Also, preferably, high
thermal-conductive hexagonal-BN (h-BN) particles not more than 1 wt% are dispersed
in copper matrix.
2) A heat-resistant nitride dispersion strengthening copper alloy consisting of, by
weight, one or two of high thermal-conductive AlN particles and high thermal-conductive
h-BN particles: 0.2 to 1.0 %, preferably 0.05 to 0.2 %, which are dispersed in a particulate
state with a grain size distribution ranging from 0.001 µm to 0.2 µm, and the balance
of copper and unavoidable impurities not more than 0.05 %.
3) A heat-resistant nitride dispersion strengthening copper alloy consisting of, by
weight, graphite whiskers: 1.0 to 10.0 %, one or two of high thermal-conductive AlN
particles and high thermal-conductive h-BN particles: 0.05 to 0.2 %, which are dispersed
in a particulate state with a grain size distribution ranging from 0.001 µm to 0.2
µm, and the balance of copper and unavoidable impurities.
4) A heat-resistant nitride dispersion strengthening copper alloy consisting of, by
weight, one of Al: 0.13 % or below and Mg: 0.09 % or below, these additive elements
being present in the form of metal oxides, one or two of high thermal-conductive AlN
particles and high thermal-conductive h-BN particles: 0.2 to 1.0 %, which are dispersed
in a particulate state with a grain size distribution ranging from 0.001 µm to 0.2
µm, and the balance of copper and unavoidable impurities.
5) A heat-resistant nitride dispersion strengthening copper alloy consisting of, by
weight, high thermal-conductive h-BN particles: 0.01 to 1.0 %, which are dispersed
in a particulate state with a grain size distribution ranging from 0.001 µm to 0.2
µm, and the balance of copper and unavoidable impurities.
[0022] The present invention is further effective in the case of containing ceramic super
fine particles alone.
[0023] In addition, the present invention relates to a method for manufacturing ceramic-particle-dispersed
metallic powder wherein metallic powder, ceramic powder, and solid lubricant powder
or solid lubricant short size fibers are put in a ceramic container along with ceramic
balls, and the ceramic container is rotated at a high rotational speed for a rotation
time enough to produce a pressing force sufficient to plastically deform the metal
powder by a centrifugal force of the ceramic balls, and also enough to uniformly disperse
the ceramic powder and the solid lubricant powder or the solid lubricant short size
fibers into the metal powder by causing the metal powder to grow to the desired grain
size larger than the original grain size thereof.
[0024] The practical manufacturing method of the present invention is as follows.
[0025] Mixed powder of copper powder and one or two of high thermal-conductive AlN particles
and high thermal-conductive h-BN particles is mechanically alloyed by using a high
energy ball mill to disperse one or two of the high thermal-conductive AlN particles
and the high thermal-conductive h-BN particles in copper matrix phase with a grain
size distribution ranging from 0.001 µm to 0.2 µm. The mechanical alloying by the
ball mill is performed by keeping a ball mill container made of ceramic or having
at least its inner wall made of copper, in which the mixed powder and ceramic ball
are put, in the temperature range of 100°C to 200°C, simultaneously de-gassing the
interior of the container to provide a pressure of 1.33·10⁻² to 1.33·10⁻³h Pa (10⁻²
to 10⁻³ torr), then replacing the container atmosphere with high purity Ar gas 99.9
wt% or more or equivalent N₂ gas under 1 atm. pressure, and thereafter effecting the
allying process at 200 to 400 rpm in rotational speed at about the room temperature
for 15 to 30 hours for the BN particles or 30 to 50 hours for other particles. Finally,
the alloyed powder is preferably annealed and purified in a stream of high purity
hydrogen gas 99.99 wt% or more. Also, preferably, the purity of the copper powder
before starting the mechanical alloying is 99.0 to 99.9 wt% and the mean grain size
thereof is not more than 200 µm. Further, preferably, the mean grain size of the high
thermal-conductive AlN particles and the high thermal-conductive h-BN particles before
starting the mechanical alloying is not more than 0.1 µm, the purity thereof is 99.2
wt% or more, and the thermal conductivity of powder particles in the form of a sintered
body is not less than 150 W/m·K for the AlN particles and not less than 50 W/m·K for
the BN particles.
[0026] Alternatively, the heat-resistant nitride dispersion strengthening copper powder
of the present invention is manufactured in such a manner that mixed powder of copper
powder, graphite whiskers and one or two of high thermal-conductive AlN particles
and high thermal-conductive h-BN particles is mechanically alloyed by using a high
energy ball mill to disperse one or two of the high thermal-conductive AlN particles
and the high thermal-conductive h-BN particles in copper matrix phase with a grain
size distribution ranging from 0.001 µm to 0.2 µm. The mechanical alloying by the
ball mill is performed similarly to the above method. Preferably, the thermal conductivity
of the graphite whiskers before starting the mechanical alloying is not less than
1000 W/m·K, and the size thereof 0.3 µm to 2 µm in diameter and 1 µm to 100 µm in
length.
[0027] Alternatively, the heat-resistant nitride dispersion strengthening copper powder
of the present invention is manufactured in such a manner that mixed powder of one
of Cu - Al and Cu - Mg low alloy powder and one or two of high thermal-conductive
AlN particles and high thermal-conductive h-BN particles is mechanically alloyed by
using a high energy ball mill to disperse one or two of the high thermal-conductive
AlN particles and the high thermal-conductive h-BN particles in copper matrix phase
with a grain size distribution ranging from 0.001 µm to 0.2 µm. The mechanical alloying
by the ball mill is performed similarly to the above method.
[0028] In addition, the present invention relates to a method for manufacturing ceramic-particle-dispersed
metallic powder comprising the first step of mechanical alloying metallic raw material
powder and ceramic powder to produce metallic powder in which the ceramic particles
are dispersed, and the second step of mechanical alloying the metallic powder in which
the ceramic particles are dispersed and solid lubricant powder or solid lubricant
short size fibers.
[0029] As an alternative, the present invention relates to a method for manufacturing ceramic-particle-dispersed
metallic powder comprising a first step of mechanically alloying metallic powder and
solid lubricant powder or solid lubricant short size fibers, and a second step of
mechanical alloying the metallic powdery produced by the first step and ceramic powder.
[0030] Further, the present invention relates to ceramic-particle-dispersed composite metallic
powder in which ceramic super fine particles and solid lubricant particles or solid
lubricant short size fibers are embedded in metallic powder, wherein the composite
metallic powder contains the particles not less than 40 wt% of which grain size is
not less than 60 µm.
[0031] The ceramic-particle-dispersed metallic powder according to the present invention
can be manufactured by any of the above-mentioned methods, and is provided as satisfying
the essential requirements for the metallic members mentioned before.
[0032] Further, the present invention relates to a ceramic-particle-dispersed metallic member
which is manufactured by sintering the ceramic-particle-dispersed metallic powder
at a high temperature under a pressure.
[0033] The practical sintering process is carried out as follows.
[0034] Thus, the manufacturing method of the invention comprises a step of mechanical alloying
mixed powder of metallic powder, ceramic powder and solid lubricant particles or solid
lubricant short size fibers, more preferably mixed powder of a matrix powder made
of high purity copper, copper, high thermal-conductive copper containing graphite
whiskers or a copper alloy, and one or two of high thermal-conductive AlN particles
and high thermal-conductive h-BN particles, or a step including the above step and
a purifying process for the alloyed powder; a step of filling the mechanically alloyed
powder in a metallic container; a step of de-gassing the interior of the container
and then sealing up it; a step of sintering the sealed-up powder by applying predetermined
plastic deformations under a hot hydrostatic pressure or by thermal extrusion; and
a step of carrying out final heat treatment or working. According to the above method,
a metallic member having superior characteristics such as high electric conductivity,
high thermal conductivity, heat resistance, wear resistance and neutron irradiation
resistance, can be manufactured.
[0035] Primary uses of the metallic member obtained by the above manufacturing method are
as follows.
[0036] The present invention is of a fluid processing apparatus in which a plurality of
through holes are formed in a cylinder block which is fixed to a rotary shaft supported
by a stationary member, a cylinder head is disposed to enclose an open end face of
the cylinder block, pistons are disposed at one ends respectively in the through holes
of the cylinder block, the other ends of the pistons are pivotably held by a rotary
plate disposed to face the cylinder block, spacers are disposed to support the rotary
plate for driving the pistons, and the cylinder block is rotated to reciprocally move
the pistons for sucking, compressing and delivering a working fluid, wherein the cylinder
block and the rotary plate are each made of an aluminum base alloy in which ceramic
super fine particles, and solid lubricant particles or solid lubricant short size
fibers are dispersed.
[0037] The invention is of also a compressor comprising a wobble plate fixed to a rotary
shaft and a piston reciprocally moving through a sliding member with rotation of the
wobble plate, wherein at least one of the wobble plate, the sliding member and the
piston is made of a copper base sintered alloy in which ceramic super fine particles,
and solid lubricant particles or solid lubricant short size fibers are dispersed.
[0038] The invention is of also a vacuum circuit breaker comprising a fixed electrode, a
movable electrode disposed to be able to approach or to move away from the fixed electrode
in opposite relation, and an insulating case containing both the electrodes under
vacuum, wherein both the electrodes are each made of a copper base sintered alloy
in which ceramic super fine particles, and solid lubricant particles or solid lubricant
short size fibers are dispersed.
[0039] The present invention relates to a pantograph contact strip made of an aluminium
base sintered alloy in which ceramic super fine particles, and solid lubricant particles
or solid lubricant short size fibers are dispersed.
[0040] Practical combinations of the composition and use of the metallic member according
to the present invention are as follows.
[0041] The invention is of a heat-resistant spot welding electrode which is formed of a
nitride dispersion strengthening copper alloy consisting of matrix made of one of
copper and a copper alloy, and one or two of high thermal-conductive AlN particles
and high thermal-conductive h-BN particles dispersed in the matrix phase to increase
heat resistance of the matrix, and is of also a spot welder using the electrode.
[0042] Further, the invention is of wear-resistant materials for sliding contact members
and electric contact materials which are formed of a nitride dispersion strengthening
copper alloy consisting of copper or a copper alloy, high thermal-conductive graphite
whiskers, and one or two of high thermal-conductive AlN particles and high thermal-conductive
h-BN particles.
[0043] Still further, the invention is of a circuit breaker or switch for use in vacuum
or air of which electrode members are formed of a nitride dispersion strengthening
copper alloy consisting of high thermal-conductive graphite whiskers, and one or two
of high thermal-conductive AlN particles and high thermal-conductive h-BN particles
dispersed to increase heat resistance and depositing resistance.
[0044] Metallic powder subjected to alloying in the present invention can be obtained by
the following method. Thus, high purity metallic powder is preferably manufactured
by preparing a high purity metal and a high purity alloy as raw fine powder materials,
using an image furnace or a laser beam as a heat source for melting a high purity
metal wire and a high purity alloy wire both continuously supplied, and jetting a
gas mixture of high purity hydrogen 99.99 wt% or more and high purity Ar 99.9 wt%
or more, as atomizing gas, to the melting region through a gas nozzle at a flow rate
ratio of "30 to 50" : "70 to 50" under a high pressure or under a reduced pressure
created by evacuation, thereby producing high purity metallic fine powder under an
atomized reducing atmosphere.
DETAILED DESCRIPTION OF THE INVENTION
[0045] The ceramic super fine particles used in the present invention are finely dispersed
to strengthen the mother phase of a matrix metal, enabling the solid lubricant particles
or solid lubricant short size fibers to be positively held in the matrix. The solid
lubricants can be thereby surely prevented from breaking away from the matrix during
sliding operations and, as a result, superior sliding contact characteristics can
be for a long term. The above effect cannot be achieved unless the ceramic particles
dispersed for strengthening are finer than at least the solid lubricants.
[0046] More specifically, the satisfactory strengthening effect cannot be achieved unless
the mean grain size of the ceramic particles is 200 nm or below. Smaller ceramic super
fine particles are more preferable from the viewpoint of the strengthening effect,
but requires a longer time for the mechanical alloying. For this reason, the preferable
mean grain size of the ceramic particles is 1 to 100 nm. While the strengthening effect
is obtained at the smaller content by finer dispersion, the content of the ceramic
particles is preferably 0.01 to 1.0 wt%, more preferably 0.03 to 0.3 wt%.
[0047] The ceramic powder used in the present invention is one or two of an oxide, nitride,
carbide and boride. Particularly preferable ceramic is one or more selected from Al₂O₃,
ZrO₂, MgO, CrN, ZrN, SiO₂, TiO₂, AlN, TiB₂, ZrB₂, BN, B₄C, β-SiC, TiC, TiN and NbC
which are less reactive with Al and Cu. The ceramic powder is preferably mechanically
alloyed so as to have a grain size distribution ranging from 0.001 µm to 0.02 µm in
the dispersion strengthened alloy. It is also preferable to use the ceramic powder
of which mean grain size is not more than 0.1 µm before starting the mechanical alloying.
This is because the ceramic particles are pulverized into finer particles in a ball
mill, but a final grain size distribution depends on the size of starting particles.
The necessity that the target grain size distribution be in the range of 0.001 µm
to 0.02 µm is deduced from considerations that a lower limit in pulverization by the
mechanical alloying is 0.001 µm order, and that effective resistivity against location
is obtained at about 0.02 µm in maximum. In particular, the grain size distribution
is preferably not more than 0.01 µm. Also, for the purposes of keeping the ceramic
particles hard to react with Al or Cu matrix and maintaining high purity of Al or
Cu matrix, it is preferable to use high purity ceramic which does not contain other
metals. Taking into account the industrial productivity, the purity of the ceramic
particles is preferably not less than 99.0 %. Above all, AlN and h-BN are preferable
because of being much less reactive with Al and Cu.
[0048] A base metal is preferably of Cu, Al, Fe, Ni, Co, Ti, etc. which are usually as structural
materials. Such a base metal may be an alloy containing another element.
[0049] A description will now be given of copper as a base metal.
[0050] Copper and nitrogen are elements hard to react with each other. A direct coupling
reaction between nitride ceramic and copper is also hard to occur. AlN and h-BN, particularly,
for use in the nitride dispersion strengthening copper alloy of the present invention
are poor in wetting property with other metals. Further, nitride and other metals
are even less reactive with each other as the nitride has higher purity. It is therefore
possible to prevent impurities from dispersing in copper matrix, i.e., prevent a lowering
in purity of the copper matrix. Thus, using high purity AlN or BN 99.2 wt% or more
as dispersion particles results in the improved strength of copper matrix at high
temperature. The use of such dispersion particles also ensures stability of the particles
and will not deteriorate excellent characteristics, i.e., high electric conductivity
and high thermal conductivity, intrinsic to copper as matrix. High purity AlN or BN
has high thermal conductivity and hence contributes to an improvement in thermal conductivity
of the particle dispersed copper alloy member to a greater extent than using other
ceramic particles which are not so thermal-conductive. The powder purity is preferably
99.2 wt% or more for each of AlN and h-BN. It is also desired that the AlN and BN
powder having purity in the above range exhibit thermal conductivity not less than
150 W/m·K and 50 W/m·K, respectively.
[0051] A mechanism for increasing the strength of the particle dispersed copper alloy is
attributable to the effect of dispersed particles to prevent dislocation movement
that is responsible for plastic deformations of matrix (i.e., the kinetic dislocation
pinning effect). The finer are dispersed particles and the shorter is the spacing
between the dispersed particles, the greater will be the pinning effect. However,
the reduced spacing between the dispersed particles resulted from the finer dispersed
particles increases the location preventing ability so drastically that plastic deformations
are hard to occur.
[0052] Therefore, the spacing between the dispersed particles requires adjustment, but that
spacing is strongly dependent on the rate of the dispersed particles added and is
also affected by the initial grain size, a degree of pulverization of particles by
the ball mill, and aggregation of particles during the manufacturing.
[0053] In view of the above, the grain size of the dispersed particles is preferably 0.001
µm to 0.2 µm in order to provide satisfactory workability and toughness of the dispersion
strengthened alloy. Where h-BN particles are added to improve the strength and wear
resistance, the strength can be increased by super fine particles and the wear resistance
can be improved by large particles having the grain size not less than 0.25 µm. Accordingly,
a grain size distribution in entirety is 0.001 µm to 10 µm. In this case, the content
of super fine particles is preferably not more than 1.0 wt% and the content of large
particles is preferably 1 to 10 wt%.
[0054] According to the present invention, the mean grain size and the content of the ceramic
super fine particles are not more than 200 nm and 1 wt%, respectively, and the ceramic
particles are dispersed not less than 500 in number per section area of one square
micrometer at 1 wt% substantially over the entirety region of the alloy, the number
of the dispersed ceramic particles depending on the content. In particular, the number
of the ceramic particles dispersed per section area of one square micrometer is preferably
not less than 500, more preferably not less than 1000, at 0.001 wt%. While the mean
spacing between the ceramic particles varies depending on the content, it is preferably
set to any value on or below the straight line interconnecting a point E (0.01 %;
100 nm) and a point F (1.0 %; 10 nm), more preferably on or below the straight line
interconnecting a point G (0.01 %; 50 nm) and a point H (1.0 %; 5 nm), when plotted
in the logarithmic scale as mentioned before.
[0055] Thus, the present invention is to strengthen the mother phase of the matrix metal
by dispersing ceramic super fine particles under specific conditions. As a result,
the content of the ceramic super fine particles can be held at a trace amount and,
therefore, thermal and electric characteristics of the matrix metal will not be significantly
degraded by the strengthening.
[0056] Used as the solid lubricants are graphite powder, graphite whiskers, carbon fibers,
BN powder, W₂S, Mo₂S and so on. The grain size of the solid lubricants dispersed in
a powdery state in the matrix metal is 0.25 to 10 µm. The whiskers or fibers are preferably
0.25 to 10 µm in diameter and not more than 500 µm, more preferably 100 µm, in length.
The content of the solid lubricants is preferably 0.5 to 10 wt%, more preferably 1
to 5 wt%.
[0057] The mechanical alloying by using a high energy ball mill progresses such that particles
of a matrix metal powder is plastically deformed and flattened with impact energy
produced between balls moving in the mill or between the balls and the container wall,
and ceramic particles and solid lubricants are embedded in each of the particles during
the repeated processes of compressing pulverization and shearing attrition. Accordingly,
while the melting process has difficulties in dispersing ceramic particles because
of decomposition thereof, the present invention enables ceramic powder to be dispersed
in and alloyed with the matrix metal on nano-meter order even at low temperatures
nearly the room temperature by the above mechanical alloying process. In order to
prevent impurities from entering and contaminating the metal matrix from the balls
and the container as far as possible during the mechanical alloying, it is desired
that any other metal than that as the base material is not used for the balls and
the container. For this reason, the balls and the container are preferably made of
a hard ceramics. In practice, preferably, the balls are made of ZrO₂ which has high
toughness and high specific gravity, and the container is made of ZrO₂ likewise, or
at least its inner wall is made of the same metal as the base material (copper to
copper, for example) but having purity of 99.9 wt%. In the case of using Attoritor
(a tradename of Attoritor Union Process Co.), a rotary shaft and an agitator located
in the container are preferably coated with a liner made of comparable copper. Achieving
satisfactory alloying requires not only high impact energy, but also an improvement
of the alloying efficiency. To satisfy these requirements, it is preferable that the
ratio of mixed powder weight to ball weight is 1/10 to 1/20 for Attoritor and 1/5
to 1/10 for a planetary type ball mill, and the rotational speed of the ball mill
is 200 to 400 rpm. The mechanism of embedding (alloying) ceramic powder or solid lubricant
particles in metallic powder, especially, such that the ceramic powder can be homogeneously
dispersed in the super fine grain size preferably not more than 0.2 µm, is realized
by increasing the grain size of alloy powder produced the mechanical alloying. This
is achieved under the condition that the alloy powder contains the particles not less
than 40 wt% of which grain size is not less than 60 µm.
[0058] It is believed that alloying of nitride particles occurs rapidly because of the use
of soft copper powder, but at least 10 hours or more is required for more homogeneous
and finer dispersion. Therefore, the alloying time is preferably relatively short,
in particular 15 to 30 hours, for sliding contact materials added with h-BN in which
a grain size distribution including large particles is required as mentioned before,
and for sliding contact and electric contact materials made of a copper alloy containing
graphite whiskers in which those whiskers are to be prevented from pulverizing into
finer size. In other cases, the longer alloying time, i.e., 30 to 50 hours, is desired
for still more homogeneous and finer dispersion. As a pretreatment before starting
the alloying, the interior of the container is preferably baked at 100 to 200°C for
30 to 60 minutes under 1.33·10⁻² to 1.33·10⁻³h Pa (10⁻² to 10⁻³ torr) in order to
prevent from mixing as far as possible. Particularly, where high purity copper powder
is used, the container is preferably baked under a high vacuum of 1.33·10⁻⁴ to 1.33·10⁻⁵
h Pa (10⁻⁴ to 10⁻⁵ torr). For the purpose of avoiding contamination by oxygen to the
fullest possible, the atmosphere is preferably formed by high purity Ar gas 99.9 wt%
or more under 1013 h Pa (1 atm.) pressure or equivalent N₂ gas. Particularly, in the
case of requiring more purification of powder produced by the mechanical alloying,
the powder is preferably heat-treated in an atmosphere of hydrogen. More specifically,
it is preferable that the heat treatment is made at the purifying temperature of 700
to 900°C in a stream of high purity hydrogen gas 99.99 wt% or more purified by using
Pd.
[0059] The dispersion alloyed powder is sintered by the thermal extrusion, HIP (Hot Isostatic
Pressing) or hot pressing process after filling the alloyed powder in a container
made of the same metal as the base metal. Taking into account diffusing fusion and
densification of the alloyed powder, the sintering is preferably carried out in the
range of 600 to 800°C for Cu or Cu alloys of the base material, 500 to 650°C for Al
or Al alloys of the base material, and 1000 to 1150°C for Fe or Fe alloys of the base
material. As a pretreatment before starting the sintering, the container evacuating
process is performed similarly to the above for removing adsorbed moisture, oxygen
and other impurities out of the container sequentially so that gas impurities such
as oxygen will not cause contamination during the sintering at high temperatures as
far as possible. In this case, however, the evacuation process is preferably carried
out stepwise under a vacuum of 1.33·10⁻⁴ to 1.33·10⁻⁵ h Pa (10⁻⁴ to 10⁻⁵ torr) at
100°C for 10 to 30 minutes, at 200°C for 10 to 30 minutes, and at 400°C for 30 minutes.
[0060] In the nitride dispersed copper alloy, addition of graphite whiskers is preferable
in, first, applying high lubricating property and heat resistance to the nitride dispersed
copper alloy, thereby providing suitable sliding contact materials, and secondly applying
superior low contact resistance and depositing resistance, thereby providing suitable
electric contact materials for circuit breakers, switches and so on. If the rate of
graphite whiskers added is not more than 1 vol%, the above characteristics cannot
be fully developed. But if it is not less than 10 vol%, the graphite content is too
large, resulting in that electric contact materials, for example, exhibit an inferior
arc discharge durability and toughness is generally lowered. Accordingly, the preferable
range of the graphite content is 1 to 10 %. It is desired that graphite whiskers used
are highly thermal-conductive and in the form of fibers having a smaller diameter.
In other words, graphite whiskers being properly finely and homogeneously dispersed
and oriented at random by the mechanical alloying makes it possible to efficiently
improve thermal conductivity of the mechanically alloyed copper alloy, wear resistance
of the alloy surface, and further an arc discharge durability for higher erosion resistance.
For that reason, higher thermal conductivity of the graphite whiskers is more preferable.
Taking into account the industrial productivity, the graphite whiskers preferably
have thermal conductivity not less than 1000 W/m·K, a diameter of 0.3 to 2 µm, and
a length of about 100 µm maximally.
[0061] In consideration of the target strength of reference and application products from
existing examples of Y₂O₃ dispersion strengthening Fe and Ni base alloys, the rate
of AlN or h-BN separated added for dispersion and the rate of AlN and h-BN both added
together is preferably 0.05 to 0.2 wt% for metallic superconducting stabilizers which
do not necessarily require high strength at the room temperature, 0.2 to 1.0 wt% heat
sink materials for the first wall diverter of a fusion reactor, lead frames for semiconductors
and integrated circuits, spot welding electrodes, and sliding contact and electric
contact materials made of a copper alloy containing graphite whiskers, which require
the high strength, particularly, at high temperatures, and 1.0 to 10 % for those sliding
contact materials in which h-BN is added as a lubricant to improve lubricating property.
[0062] In plastic deformations of a particle dispersion strengthening copper alloy, deformation
resistance has a negative temperature dependency. This is because fine dispersed particles
in nano-meter order to several tens nano-meter serve as thermal activation barriers
against dislocation. Even for metallic superconducting stabilizers in which the content
of dispersed particles is relatively low, sufficient strength can be obtained since
they are used at a very low temperature about 4.2 K. The reason why the upper limit
of the grain size distribution of copper powder for constituting a copper matrix is
set to 200 µm is as follows. If the grain size is too small, the surface area of copper
matrix to be covered would be so increased as to cause a fear that the amount of surface
oxidation occurred during the manufacturing, i.e., oxygen in copper matrix, may increase
excessively. Conversely, if the grain size is not less than 200 µm, it would be difficult
to homogeneously disperse the copper powder during the mechanical alloying. While
the copper powder is desired to be as pure as possible for the metallic superconducting
stabilisers and heat sink materials of the first wall diverter of a fusion reactor
both of which require ultimate electric conductivity and thermal conductivity, the
purity 99.9 % or more is preferable, taking into account the industrial productivity
and cost. For other above-mentioned application products except the metallic superconducting
stabilizers and heat sink materials of the first wall diverter of a fusion reactor,
the purity of the copper powder is 99.0 to 99.9 wt% in the range of usual pure copper.
Using copper added with trace amounts of Al and Mg is intended to not only fix oxygen,
unavoidably mixed during mechanical alloying, in the form of Al₂O₃ and MgO through
reactions with the added elements, but also enhance the strength by causing these
oxides to serve as barriers against dislocation. In spite of taking care to prevent
oxygen from mixing during the pretreatment oxidation of the copper surface and the
mechanical alloying, a component analysis result showed the presence of oxygen ranging
from 0.06 to 0.09 wt%, as seen from the following description of embodiments. To fix
oxygen of at least 0.06 wt%, Al and Mg are required to be added 0.13 wt% and 0.06
wt%, respectively. Therefore, Al and Mg are preferably added not more than 0.13 wt%
and 0.06 wt%, respectively, so that surplus Al and Mg will not brought into a solid-solution
state. The residual oxygen can be removed by heat-treating the alloyed powder in a
hydrogen atmosphere.
BRIEF DESCRIPTION OF THE DRAWINGS
[0063] Fig. 1 is a schematic view of a mechanically alloying apparatus.
[0064] Fig. 2 is a schematic view of a mechanically alloying apparatus.
[0065] Fig. 3 is a graph showing the relationship between an MA process time and the mean
grain size of particles.
[0066] Fig. 4a - 4c are bar graphs showing the relationship between the grain size and a
particle abundance rate.
[0067] Fig. 5 is a graph showing the relationship between the content of ceramic particles
and the mean particle spacing.
[0068] Fig. 6 is a graph showing the relationship between a surface pressure and a specific
wear.
[0069] Fig. 7 is a schematic view of a mechanically alloying apparatus.
[0070] Fig. 8a is a horizontal cross-sectional view of another mechanical alloying apparatus.
[0071] Fig. 8b is a vertical cross-sectional view of said mechanical alloying apparatus.
[0072] Fig. 9 is a sectional view of a swash-plate type compressor.
[0073] Fig. 10 is a sectional view of a compressor.
[0074] Fig. 11 is a sectional view of a vacuum circuit breaker.
[0075] Fig. 12 is a graph showing the relationship between a graphite whisker content and
a specific breakdown voltage.
[0076] Fig. 13 is a graph showing the relationship between the mean grain size of BN particles
and a specific breakdown voltage.
[0077] Fig. 14 is a schematic view of a pantograph.
Example 1
[0078] An embodiment of a method for manufacturing particle dispersion strengthened alloy
powder in which nitride, oxide or carbide particles and solid lubricants are dispersed,
according to the present invention, will be described with reference to Fig. 1. Fig.
1 is a schematic view of a mechanical alloying apparatus, showing a planetary type
ball mill. Rotations are transmitted from an external driving system 1 to a stand
frame 2 for revolving it. Simultaneously, centrifugal forces indicated by arrows 5
are produced in four attrition containers 4 disposed crosswise on the stand frame
2. The revolving stand frame 2 and the attrition containers 4 rotating their own axes
repeat opposite rotational movements to generate strong centrifugal accelerations
so that powder and balls 7 in the attrition containers 4 collide with each other at
high energy.
[0079] The attrition containers 4 each comprise, as shown in Fig. 2, cap 24 made of a copper-
or ZrO₂ provided with a vacuum-leak valve 21, an Ar or nitrogen gas inlet valve 22
and a thermocouple inlet tube 23 for measuring the temperature, container 26 made
of a copper-, Al₂O₃- or ZrO₂ having a volume of 500 cc and provided with a tape-type
heater 25 wound around the container, balls 27 made of ZrO₂ being 10 mm in diameter,
and mixed powder 28, both the balls 27 and the mixed powder 28 being put in the container
26. The balls 27 rotate along an inner wall of the container 26 while colliding with
one another and the inner wall of the container 26. Used as the cap 24 and the container
26 were ones manufactured by way of trial using oxygen-free copper (OFC) with purity
of 99.99 wt%, or commercially available ones made of Al₂O₃ or ZrO₂, and then subjected
to the mechanical alloying. In the case of using the container made of OFC, since
the strength of OFC is low, the container was manufactured by cold working and filled
with only a nitride, oxide or carbide before actually starting the mechanical alloying
so that an inner wall of the container was strengthened by dispersion of the nitride,
oxide or carbide.
[0080] The purity and the mean grain size of each of starting powders used in this embodiment
was shown in Table 1 below.
[0081] Fig. 3 is a graph showing the relationship a mechanical alloying (MA) process time
and the mean grain size of powder particles produced by using No. 1 alloy powder.
As seen from the graph of Fig. 3, it was confirmed that the mean grain size of the
alloy powder increased with the elapse of the MA process time, and this increase in
the grain size promoted a size reduction and dispersion of the ceramic and solid lubricant
particles. It is also seen that the ball pressing force is proportional to the rotational
speed, and that the alloying does not so progress at 150 rpm or below even for a long
period of time, but progresses remarkably at 200 rpm or more.
[0082] Figs. 4a - 4c are bar graphs showing a grain size distribution of the produced alloy
powder. The alphabet letters
a,
b and
c in Fig. 3 correspond to Figs. 4a - 4c, respectively. As seen from Fig. 4a, alloying
of the powder
a does not yet so progress and the alloying rate of those particles having the grain
size not less than 60 µm is only about 15 %. However, the above alloying rate increases
to 40 % or more at the powder
b (Fig. 4B) and to 60 % or more at the powder
c (Fig. 4C). From the standpoint of the alloying, in particular, the alloying rate
of those particles having the grain size not less than 60 µm is preferably not less
than 40 % as resulted at the powder
b, more preferably not less than 60 % as resulted at the powder
c.
[0083] Referring to Table 1, each mixed powder 1500 g of Cu, Al or Fe powder, one of Al₂O₃,
ZrO₂, MgO, SiO₂, TiO₂, AlN, BN, B₄C, β-SiC, TiC, and NbC powders, and graphite whiskers
was filled in the four containers along with 200 balls in a glove box under a high
purity Ar atmosphere. The balls and the interior of the ball mill container were fully
cleaned by pre-operation of the ball mill using alcohol and acetone. The mechanical
alloying process was started by replacing air in the container with high purity Ar
gas 99.99 wt% under 1 atm. pressure and sealing up the container at the time a degree
of vacuum reaches 1.33·10⁻² to 1.33·10⁻³ h Pa (10⁻² to 10⁻³)torr by evacuation and
subsequent heating at about 120°C. The rotational speed was 300 rpm and the process
time was 30 hours. After the mechanical alloying, the alloyed powder was put into
a preserving container and sealed up under a vacuum inside the aforesaid glove box.
It was found
Table 1
Powder Used |
Purity (wt%) |
Mean Grain Size (µm) |
Cu |
99.99 |
8 |
Al |
99.99 |
120 |
Fe |
99.99 |
30 |
Al₂O₃ |
99.999 |
0.05 |
ZrN |
99.9 |
0.1 |
ZrO2 |
99.9 |
0.1 |
MgO |
99.99 |
0.06 |
SiO2 |
99.99 |
0.1 |
TiN |
99.9 |
0.1 |
TiO2 |
99.9 |
0.07 |
AlN |
99.9 |
0.05 |
BN |
99.4 |
0.07 |
B4C |
99.0 |
0.1 |
CrN |
99.5 |
0.1 |
β-SiC |
99.5 |
0.08 |
TiC |
99.5 |
0.05 |
NbC |
99.0 |
0.06 |
graphite whiskers |
- |
dia. 0.5 µm |
length 10 µm |
that the alloyed powder was pulverized while deforming into the flattened form and
ceramic particles were embedded in Cu, Al or Fe powder particles, possibly as a result
of deformations and forging repeated many times. Also, ≦ 0.057 mm using (250 mesh)of
high purity Al powder each particle of which has alumina film thereon, similar mixed
powder was mechanically alloyed by the ball mill in a like manner to above. By so
mechanical alloying the mixed powder, copper oxide, alumina or ferrous oxide on the
powder surface was very finely alloyed into the metallic powder and homoge-neously
dispersed.
[0084] Described below is a sintering process for solidifying the dispersion strengthening
alloy powder thus produced. After filling the alloy powder in a container made of
Cu, Al or Fe with high purity of 99.99 wt% and having a vacuum-leak pipe inside a
glove box, the interior of the container was evacuated stepwise under a vacuum of
1.33·10⁻² to 1.33·10⁻³ h Pa (10⁻² to 10⁻³)torr at 100°C for 20 minutes, at 200°C for
20 minutes, and at 400°C for 30 minutes. After completion of the evacuation, the pipe
was pressed at two locations and the pressed pipe ends were tightly closed by TIG
(tungsten inert gas) welding. The sintering was carried out by using an HIP (hot isostatic
pressing) apparatus for 1 hour at 900°C for the Cu system powders, 600°C for Al system
powders, and 1050°C for Fe system powders. Thereafter, hot pressing was carried out
at 850°C, 550°C and 1050°C for Cu, Al and Fe system powders, respectively. An electric
resistance sample and a tensile strength test sample were prepared from each final
alloy, followed by annealing under vacuum of 2.67 to 5.33·10⁻⁸ h Pa (2 to 4 x 10⁻⁸)torr
for 1 hour at 900°C, 600°C and 1200°C for Cu, Al and Fe system powders, respectively.
A resistance value as electric characteristics, thermal conductivity, and the yield
strength at the room temperature were measured. The composition and measured results
of each of the dispersion strengthened alloys are shown in Table 2. It was confirmed
that the alloys of the present invention had the high strength, large thermal conductivity,
and low electric resistance values.

[0085] Fig. 5 is a graph showing, in a logarithmic scale, the relationship between the mean
spacing and the content of dispersed ceramic particles. In this embodiment, the diameter
of the ceramic particles dispersed in the pure metal was not more than 0.02 µm and
most of the particles, i.e., about 95 % or more in number, was 0.002 to 0.008 µm (mean
value: 0.005 µm). Considering that fine and homogeneous dispersion of ceramic super
fine particles in metal crystal grains provides the strengthening, elongation and
superior electric characteristics, the mean spacing between the dispersed particles
was measured as in index of dispersion in this embodiment. The data shown in Fig.
5 at the contents of 0.01 %, 0.25 %, 0.5 % and 1.0 % are values resulted for the Al
system members containing 5 vol% graphite whiskers. As will be seen, as the ceramic
content increases, the mean spacing is reduced and Al is strengthened correspondingly.
In this embodiment, the mean spacing between the ceramic super fine particles was
about 2.5 nm at the content of 1.0 wt%, about 3.5 nm at 0.5 wt%, about 5 nm at 0.25
wt%, and about 25 nm at 0.01 wt%. It was also found that the number of the ceramic
particles dispersed per section area of one square micrometer at the content of 0.01
wt% was about 1500, and the number at 0.1 % and 1.0 % increased substantially proportional
to the contents. The ceramic particles were dispersed with the mean spacing as mentioned
above, the spacing value may be more or less deviated from the measured values. In
other words, the ceramic particles are preferably dispersed so that the mean spacing
falls within the rectangular region defined by straight lines interconnecting a point
A (0.01 %; 20 nm), a point B (0.01 %; 500 nm), a point C (1.0 %; 50 nm) and a point
D (1.0 %; 2 nm) as shown, more preferably on or below the straight line interconnecting
a point E (0.01 %; 100 nm) and a point F (1.0 %; 10 nm), most preferably on or below
the straight line interconnecting a point G (0.01 %; 50 nm) and a point H (1.0 %;
5 nm). The smaller mean spacing of the ceramic particles dispersed, the higher is
the strength. But setting the mean spacing to a value on or above the straight line
interconnecting the points A and D, satisfactory electric characteristics, strength,
elongation, etc. can be obtained.
[0086] Fig. 6 shows results of wearing tests made on the Cu system materials as compared
with a molten and cast alloy material. The mating material was graphite. Sliding contact
tests of No. 1 alloy sample resulted in that the specific wear was 4 x 10⁻¹⁰ (mm³/m·kg/cm²)
in the so-called dry test (surface pressure; 7 kgf/mm²) using no lubricant, 1.5 x
10⁻¹¹ (mm³/m·kg/cm²) in the test (surface pressure; 50 kgf/mm²) using water as an
lubricant, and 1 x 10⁻¹¹ (mm³/m·kg/cm²) in the test (surface pressure; 100 kgf/mm²)
using turbine oil as a lubricant.
[0087] For No. 2 alloy sample, the specific wear was 2 x 10⁻¹⁰ (mm³/m·kg/cm²) in the dry
test using no lubricants, 1.2 x 10⁻¹¹ (mm³/m·kg/cm²) in the test using water as an
lubricants, and 1 x 10⁻¹¹ (mm³/m·kg/cm²) in the test using turbine oil as a lubricant.
[0088] A curve in Fig. 6 represents data of the comparative alloy, i.e., a typical wear-resistant
copper alloy of Cu - 9Al - 0.8 Ti - 10 graphite, manufactured by the fusion alloying
process of melting and casting.
Example 2
[0089] Fig. 7 is a sectional view showing another embodiment of the mechanical alloying
apparatus. The apparatus of this embodiment is generally called Attoritor (a trade
name). The mechanical alloying is carried out as follows. Raw material powder 31 and
balls 32 as an alloying medium are both put in a mechanical alloying container 33
and are agitated by an agitator 35 having arms 34. By carrying out the above process,
particle dispersion strengthening powder was manufactured by mechanical alloying.
[0090] Additionally, the apparatus of this embodiment is provided with an external heater
36 for adjusting the alloying temperature inside the container 33. The alloyed powder
produced after the alloying process was recovered through a recovering hole 37 provided
at the container bottom.
Example 3
[0091] Figs. 8a and 8b are a horizontal and a vertical sectional views, respectively, showing
still another embodiment of the mechanically alloying apparatus. The apparatus of
Figs. 8a and 8b comprises a stationary container 41, a main shaft 42 rotating about
its axis within the container 41, and several sub shafts 45 revolving, as indicated
by arrows 44, in conjunction with rotation, indicated by arrow 43, of the main shaft
42. The subshafts 45 supported by terminal beard 50 are each provided with a number
of ring-shaped grinding media 46. A gap of several millimeters is left between an
outer periphery of the sub shaft 45 and an inner periphery of the ring-shaped grinding
medium 46 so that each ring can move freely. The ring serving as the grinding medium
revolves inside the grinding container while being pressed against an inner wall of
the container by a centrifugal force.
[0092] Particles 48 to be processed are sandwiched between the revolving grinding media
46 and the wall surface, and are subjected to attrition due to the combination of
centrifugal forces produced on the rings and rotation of the rings themselves, whereby
the mechanical alloying is developed. The grinding container has a jacket 47 through
which cooling water 49 is passed to suppress a temperature rise of the particles under
process.
[0093] It is desired that materials of the inner wall of the grinding container and the
rings as the grinding media are the same; hence the materials must be selected depending
on the raw material powder. Ceramic materials such as Al₂O₃, and ZrO₂ are preferable
for the copper and aluminum alloys, while stainless steels (JIS SUS) steel materials
are preferable for ferrous alloys.
Example 4
[0094] Fig. 9 is a sectional view of a swash-plate type compressor for car air conditioners
using the No. 4 alloy of Example 1 as the Cu base alloy according to the present invention.
In the compressor of this embodiment, a shaft 55 is rotated by operation of a solenoid
clutch, whereupon a swash-plate 57 attached to the shaft 55 is rotated together with
the shaft 55 to effect a swing motion. This swing motion causes a piston 53 to move
reciprocally. The piston 53 is provided with a sliding member 59 held in sliding contact
with the swash-plate 57. The sliding member 59 is formed of the Cu base alloy according
to the present invention mentioned above. This compressor was assembled in a car air
conditioner for an endurance test.
[0095] Test conditions were as follows; rotational speed: 5500 rpm, delivery gas pressure:
30 kgf/cm², inlet side gas pressure: 2 kgf/cm², test time: 500 hours, lubricant: polyalkylene
glycol, and coolant: R134a. For comparison, a similar endurance test was also made
on a compressor comprising a cylinder made of a B390 alloy and a piston made of "PTFE
+ 30 vol% carbon fibers + 2 vol% CaF₂".
[0096] The volumetric efficiency and total adiabatic efficiency were measured at 1 hour
and 500 hours after starting the test. The volumetric efficiency is represented by
a ratio of the theoretical volume of a cylinder bore and the delivery rate, and is
reduced if a gap occurs between the cylinder bore and the piston ring. The total adiabatic
efficiency represents a contribution rate of compressors to cooling energy as a result
of converting rotational energy into thermal energy, and is also reduced if a gap
occurs between the cylinder bore and the piston ring. Accordingly, the volumetric
efficiency and total adiabatic efficiency can be considered as indices for evaluating
durability of compressors. Thus, the smaller a reduction in the efficiency, the more
are compressors endurable. The compressor using the Cu base alloy of the present invention
had the volumetric efficiency of 60 % and the total adiabatic efficiency of 57 % even
after 500 hours. The resulting small reduction in the efficiency means superior durability
of the compressor.
[0097] On the other hand, the comparative compressor had the volumetric efficiency of 52
% and the total adiabatic efficiency of 49 % after 500 hours.
[0098] Additionally, the swash-plate 57 and the piston 53 may be formed of the Al system
alloy according to the present invention.
Example 5
[0099] Fig. 10 shows a sectional view of primary parts of one embodiment in which a sliding
contact member formed of the Al system alloy according to the present invention is
employed in a compressor. Referring to Fig. 10, a spacer 82 is disposed in a cup-shaped
shell or casing 81, and a surface of the spacer 82 held in sliding contact with a
wobble plate 83 is covered by a steel sheet (shoe disk) 84 having a surface layer
formed of synthetic resin as a main ingredient. The wobble plate 83 is formed of the
Al system alloy listed in Example 1 as No. 6 alloy. A spherical portion 86 of a piston
85 is pivotably held by the wobble plate 83, and the wobble plate 83 is rotatably
supported by a center ball 80 fitted over a rotary shaft 87. Further, a cylinder block
88 having a plurality of through holes 91 around the axis is fixed to the rotary shaft
87, and the piston 85 is fitted in each of the through holes 91 in the cylinder block
88. The cylinder block 88 can be formed of the Al system alloy as with the rotary
plate 83. A cylinder head 89 having a delivery hole to delivery compressed air therethrough
is disposed to close one ends of the through holes 91 in the cylinder block 88.
[0100] Described below is the operation of the compressor. When the rotary shaft 87 is rotated
by an internal combustion engine, for example, the wobble plate 83 and the cylinder
block 88 are rotated together, whereupon the pistons 85 move reciprocally in the cylinder
through holes 31 for sucking and compressing air. At this time, a pair of the steel
sheet 84 covering the spacer 82 and the wobble plate 83 and another pair of the cylinder
block 88 and the cylinder head 89 respectively slide with each other in synch with
the rotation of the rotary shaft 87. Since these sliding motions are effected at a
high speed while being additionally subjected to a pressure produced upon compressing
air, the compressor operates under a high-speed, high-load sliding condition. Such
a high-speed, high-load sliding condition makes it difficult to sufficiently supply
a lubricant and hence may leads to boundary lubrication or no-lubrication. Therefore,
the sliding contact surfaces are preferably formed of self-lubricating materials.
In this embodiment of the present invention, since the material contains lubricant
particles fixed therein, there is no fear of seizure even if the sliding contact surfaces
are brought into a state of boundary lubrication or no-lubrication.
[0101] The compressor of this embodiment was assembled in a car air conditioner for an endurance
test. Test conditions were as follows; rotational speed: 5500 rpm, delivery gas pressure:
29 kgf/cm², inlet side gas pressure: 2 kgf/cm², test time: 200 hours, lubricant: polyalkylene
glycol, and coolant: R134a. For comparison, a compressor having a cylinder block and
a wobble plate each formed with a usual anode oxidation layer was also subjected to
an endurance test under the same conditions.
Example 6
[0102] Fig. 11 shows the structure of a vacuum valve using the No. 2 Cu system alloy listed
in Example 1 as electrode material, the vacuum valve being subjected to a circuit
breaking (or closing) characteristic test. The vacuum valve has a container composed
of a cylindrical ceramic insulating case 63 and stainless terminal boards 64 and 65,
the interior space of the container being kept at a high vacuum on the order of 1.33·10⁻⁶
to 1.33·10⁻⁸ h Pa (10⁻⁶ to 10⁻⁸ torr). Within the container are disposed a pair of
electrodes formed of the electrode material according to the present invention, i.e.,
a fixed electrode 68 fixed on a pedestal 61 and a movable electrode 69 fixed on another
pedestal 62 arranged movably through a bellows 66. These electrodes are each comprised
of an electrode portion and a support member for the electrode portion. A cylindrical
shield 67 is disposed so that when the electrode structural member is evaporated and
scattered upon breaking arcs, the shield 67 prevents the scattered material from depositing
onto an inner wall of the insulating case 63. The electrode portions of both the electrodes
61, 62 in this embodiment were formed of the No. 2 Cu base alloy listed in Example
1, and machined into the size 20 mm in diameter and 5 mm thick, followed by evaluation
tests below.
[0103] Of various electric tests, the breakdown voltage test was made by breaking off AC
300 A ten times, then applying an impulse voltage while incrementing the voltage in
a step of 5 kV, and measuring the discharge voltage values at the time insulation
breakdown occurs between the electrodes.
[0104] The breaking performance test was made by using the electrode of being 20 mm in diameter,
breaking off an AC current while incrementing it in a step of 500 A, and measuring
the critical current value at which breaking-off was disabled. Further, the cut-off
current test was made by breaking off a small AC current of 2 to 8 A, measuring the
produced cut-off current 100 times, and determining the maximum value and the mean
value of the cut-off currents.
[0105] Fig. 12 is a graph showing measured results of breakdown voltage characteristics
of the electrodes formed by the present invention, as the relationship between a specific
breakdown voltage and a content of BN particles. Also, Fig. 13 is a graph showing
the relationship between a specific breakdown voltage and the grain size of dispersed
BN particles. The specific breakdown voltage is indicated as a relative value on the
basis of a reference (1.0) corresponding to the breakdown voltage which is resulted
by using a 50 wt% Cu - 50 wt% Cr alloy as the typical conventional material. As will
be seen, the material containing the dispersed BN particles not more than 0.2 µm exhibits
the breakdown voltage in excess of that of the conventional material. Particularly,
superior breakdown voltage characteristics are achieved with the dispersed BN particles
being 1 to 10 nm in grain size.
Example 7
[0106] Fig. 14 is a front view of a pantograph for railway vehicles using, as a sliding
contact member, the No. 2 Cu base alloy of the present invention listed in Example
1. The pantograph is arranged such that a contact strip 71 is fixed by bolts to a
body (collector shoe) 73 made of an Al alloy (duralumin base alloy), and the collector
shoe 73 is fixed through insulators 74 to a mount connected to the vehicle. The collector
shoe 73 is supplied with electric power through a lead wire 75. A trolley wire 72
moves to the left and right while the vehicle is traveling, so that the wire 72 will
not come into slide contact with the surface of the contact strip 71 at the same position
at all times.
[0107] The pantograph of this embodiment can be adapted for a tendency toward higher speeds
in railways due to its high strength, high wear resistance and high electric conductivity.
Thus, the pantograph is suitable for not only the current bullet trains traveling
at 220 km/h, but also future bullet trains traveling a higher speed of 350 to 450
km/h.
[0108] As is described above, according to the present invention, there is provided a metallic
member having high strength and high wear resistance, which is very advantageous when
used as a sliding contact member in compressors and so on. Also, by using a pure metal
free from any alloy elements as a base metal, the obtained metallic member has superior
characteristics such as high strength, high thermal conductivity, high electric conductivity,
and high wear resistance; hence it is also very advantageous when used in electrodes
of vacuum circuit breakers, contact strips of pantographs, etc.
1. A ceramic-particle-dispersed metallic member in which ceramic super fine particles,
and solid lubricant particles or solid lubricant short size fibers are dispersed,
wherein the mean grain size of said ceramic super fine particles is smaller than the
mean grain size of said solid lubricant particles or the mean diameter of said short
size fibers.
2. A ceramic-particle-dispersed metallic member according to claim 1, wherein the mean
grain size of said ceramic super fine particles is not more than 200 nm, and the mean
grain size of said solid lubricant particles or the mean diameter of said short size
fibers is in the range of 0.25 to 10 µm.
3. A ceramic-particle-dispersed metallic member according to claim 1, wherein the mean
grain size of said ceramic super fine particles is not more than 200 nm, and a region
where said ceramic super fine particles are dispersed not less than 500 in number
per section area of one square micrometer is formed substantially over the entirety
region of said metallic member.
4. A ceramic-particle-dispersed metallic member according to claim 1, wherein said ceramic
super fine particles have the content not more than 1 wt% and the mean grain size
not more than 200 nm, and a region where said ceramic super fine particles are dispersed
not less than 500 in number per section area of one square micrometer at 1 wt% is
formed substantially over the entirety region of said metallic member.
5. A ceramic-particle-dispersed metallic member according to claim 1, wherein said ceramic
super fine particles have the content not more than 1 wt% and the mean grain size
not more than 200 nm, and a region where said ceramic super fine particles are dispersed
not less than 500 in number per section area of one square micrometer is formed substantially
over the entirety region of said metallic member.
6. A ceramic-particle-dispersed metallic member according to claim 1, wherein said ceramic
super fine particles have the content not more than 1 wt% and the mean grain size
not more than 200 nm, and when a relationship between the content (wt%) and the mean
particle spacing (nm) of said ceramic super fine particles is plotted in a logarithmic
scale, said relationship is distributed within the rectantular region defined by straight
lines interconnecting a point A (0.01 %; 20 nm), a point B (0.01 %; 500 nm), a point
C (1.0 %; 50 nm) and a point D (1.0 %; 2 nm).
7. A ceramic-particle dispersed metallic member according to anyone of claims 1 to 6,
wherein ceramic super fine particles and graphite whiskers are dispersed in copper,
aluminum or iron, and said metallic member is of a sintered body.
8. A ceramic-particle-dispersed metallic member according to anyone of claims 1 to 7,
wherein said metallic member is of a sintered body.
9. A ceramic-particle-dispersed metallic member according to anyone of claims 1 to 8,
wherein said metallic member constitutes a member held in sliding contact with a mating
member.
10. A method of manufacturing ceramic-particle-dispersed metallic powder, wherein metallic
powder, ceramic powder, and a solid lubricant powder or solid lubricant short size
fibers are put in a ceramic container (26) along with ceramic balls (27), and said
ceramic container is rotated at a high rotational speed for a rotation time enough
to produce a pressing force sufficient to plastically deform said metal powder by
a centrifugal force of said ceramic balls (27), and also enough to uniformly disperse
said ceramic powder, and said solid lubricant powder or said solid lubricant short
size fibers into said metal powder by causing said metal powder to grow to the desired
grain size larger than the original grain size thereof.
11. Ceramic-particle-dispersed composite metallic powder in which ceramic super fine particles,
and solid lubricant particles or solid lubricant short size fibers are embedded in
metallic powder, wherein said composite metallic powder contains the particles not
less than 40 wt% of which grain size is not less than 60 µm.
12. A ceramic-particle-dispersed metallic member according to anyone of claims 1 to 7,
wherein said metallic member is of powder.
13. A method of manufacturing a ceramic-particle-dispersed metallic member according to
claim 11 or 12, wherein said metallic powder in which ceramic super fine particles,
and solid lubricant particles or solid lubricant short size fibers are embedded, is
sintered at a high temperature under a pressure.
14. A method of manufacturing ceramic-particle-dispersed metallic powder, comprisisng
the first step of mechanical alloying metallic raw material powder and ceramic powder
to produce metallic powder in which said ceramic particles are dispersed, and the
second step of mechanical alloying said metallic powder in which said ceramic particles
are dispersed and solid lubricant powder or solid lubricant short size fibers.
15. A method of manufacturing ceramic-particle-dispersed metallic powder, comprising the
first step of mechanical alloying metallic powder, and solid lubricant powder or solid
lubricant short size fibers, and the second step of mechanical alloying said metallic
powder produced by said first step and ceramic powder.
16. A fluid processing apparatus in which a plurality of through-holes are formed in a
cylinder block which is fixed to a rotary shaft supported by a stationary member,
a cylinder head is disposed to enclose an open end face of said cylinder block, pistons
are disposed at one ends respectively in the through-holes of said cylinder block,
the other ends of said pistons are pivotably held by a rotary plate disposed to face
said cylinder block, spacers are disposed to support said rotary plate for driving
said pistons, and said cylinder block is rotated to reciprocally move said pistons
for sucking, compressing and delivering a working fluid, wherein said cylinder block
and said rotary plate are each made of an aluminum base alloy in which ceramic super
fine particles, and solid lubricant particles or solid lubricant short size fibers
are dispersed.
17. A compressor comprising a wobble plate (57) fixed to a rotary shaft (55) and a piston
(53) reciprocally moving through a sliding meber (59) with rotation of said wobble
plate (57), wherein said sliding member (59) is made of a copper base sintered alloy
in which ceramic super fine particles, and solid lubricant particles or solid lubricant
short size fibers are dispersed.
18. A vacuum circuit breaker comprising a fixed electrode (68), a movable electrode (69)
disposed to be able to approach or to move away from said fixed electrode (68) in
opposite relation, and an insulating case (63) containing both said electrodes (68,
69) under vacuum, wherein both said electrodes (68, 69) are each made of a copper
base sintered alloy in which ceramic super fine particles, and solid lubricant particles
or solid lubricant short size fibers are dispersed.
19. A pantograph contact strip (71) made of an aluminum base sintered alloy in which ceramic
super fine particles, and solid lubricant particles or solid lubricant short size
fibers are dispersed.
20. A compressor for a freezer and/or air conditioner and/or a heat exchanger, wherein
a wear-resistant member (83) made of an aluminum base sintered alloy, in which ceramic
super fine particles, and solid lubricant particles or solid lubricant short size
fibers are dispersed, is used for a bearing or a sliding contact member.